The filter wheels will contain the usual narrow band and JHK filters and two
non standard broad band filters (see below) which will exploit the short
wavelength sensitivity of the instrument. UFTI is expected to be at least as
sensitive as IRCAM-3 in the 1-2.5 micron range. We anticipate that
\it{the greatest gains in sensitivity will be in the K band} \rm, since UFTI has
no warm mirror surfaces, unlike IRCAM-3 which employs two warm external folding
and collimating mirrors. IRCAM-3 will remain available for operation at
3-5 microns.
September Update
The instrument was shipped to Hawaii on September 2nd, with the
replacement science grade array installed and fully functional. A dark frame and
a flatfield of the new chip are shown below, illustrating the almost total
absence of large scale structure in the flatfield. Tests of the new array in
August indicate that its performance is very similar to the previous array in
terms of linearity, well depth and dark current (except for the dark glow fault,
which is absent!). Commissioning at UKIRT is now scheduled for 29th September to
8th October. The last remaining hardware problem: dewing of the large cryostat
window, has been solved by attaching a small commercial fan next to the window.
This provides a steady flow of air across the glass, preventing build up of
moisture.
Filter Update
We have ordered 2 unconventional
filters from Barr, which are due to be delivered in October, in time for
commissioning we hope. These are a broad band Z filter (0.85-1.05 um half power
points) and a long I filter which operates from 0.78 um to 0.93 um. The short
wavelength limit is determined by the QE of the array, which has a sharp edge at
786 nm. The Z filter operates in a region of low sky background, where OH
emission is low compared to the other infrared passbands. The I filter operates
in a region of even lower OH glow and avoids both the strong atmospheric
absorption feature at 0.76 um and a weak but variable water feature at 0.93-0.98
um.
August Update
UFTI was
taken to the Astronomy Technology Centre at ROE in June for acceptance testing.
The VMS and EPICS softare integration was successful but a serious hardware
problem with the science grade array detector was discovered. This has delayed
the planned commissioning period in August to the end of September/early
October. The problem was a low level glow in one quadrant of the array which we
had attributed to a subtle light/heat leak during the previous month of testing.
However, this consistent glow, which appears to be a reflection, persisted
despite all efforts to eradicate a leak. (It is just visible as a faint arc near
the bottom of the flatfield image of the science array, slightly left of
centre.) After reinstalling the engineering array, which is very weakly
sensitive in the area of the glow, we realised that the problem was not a leak
but a property of the science array. The glow is most likely due to a hot
bonding wire, which was not detected by the manufacturer (Rockwell) who did not
dark test the device. Rockwell have agreed to supply a new science array free of
charge, delivery due in mid-August.
The regrettable delay in
commissioning has had some compensations. The new array has a smoother and
flatter flatfield response than the defective array and fewer physical defects.
The delay has also allowed us to track down some niggling but non-critical
problems with the AstroCam array controller. With the engineering array the
control system now yields a read noise of 8-10 electrons per read at 300 kHz,
which is as good as the intrinsic specification of these HAWAII arrays and six
times better than the InSb array in IRCAM-3. At 1 MHz the noise is approximately
20 electrons per read.
Dark frame, 200 s exposure at 80 K. The hot pixels are not
saturated and the dark current in other pixels is too low to be meaured, i.e.
less than 0.02 electrons per second.
Flatfield. K Band, 8s. The response of the array is so
uniform that flatfield variations are almost imperceptible. A very faint
brightening is visible in the first few dozen rows of each quadrant, which is a
readout feature which does not always subtract off perfectly. There is a small
region of dead pixels at the bottom right edge of the array. This area is small
enough to lie within the overlap region of a typical imaging mosaic.
Side view of the cryostat.
Further assembly
Detector block and array.
As above, with copper radiation shield attached.
Completed instrument in June, with Rosie demonstrating.
Collimator mirror tube
Bare Optical Bench, end view.
Optical Bench, diagonal view. Right:Array mounted on the unanodised block and backplate
of the detector box. Left: The anodised array block, upside down, showing
heating resistor and temperature sensor. 2.44 um narrow band image of a respectable astrophysicist.
The image was taken with the replacement science grade array and has been
flatfielded. 4s integration.
H Band images, not flatfielded.
K band images showing the full array, dark subtracted but
not flatfielded.
Side view of the half-painted cryostat showing the entry
window in front and the blue tube housing the collimator mirror at the lower
rear. The aluminium cryo-cooler is seen at the upper rear.
Cryostat, opposite
side
View down the collimator tube from
the telescope focal plane, as seen by light entering the camera. The folding
mirror and 1st filter wheel are seen in reflection.
Empty cryostat, bottom
half, showing the multilayer superinsulating foil.
Optical table, end view.
Optical Bench over the cryostat, in position to attach internal cable
connections for array, temperature sensors, heating resistors and
motors.
Bare Optical Bench,
underside view.
Optical Bench,
horizontal view.
Front view, also showing the yellow entry
ports for the electrical connections.
Rear view. The red, silver and black
attachments to the blue collimator tube are the pressure gauge and vacuum pump
tubes respectively.
Copper braids (left) and rear radiation
shield (right). The braids provide a flexible thermal link between the camera
and the cryostat cold-head.
Optical bench and (behind) the main
radiation shield and inner tube housing the collimator mirror. The motors which
drive the filter wheels are in place but the array housing, which will sit at
the left, was yet to be added.
First Light with the Engineering Array. The
image shows an integration of 2s taken after the first cool-down of the
instrument, operating at approx. 100 K. The cross wires are located near the
telescope focal plane and display sharp edges. More than half of the engineering
array appears to be of science quality, indicating possible usefulness in a
spectrometer.
First Light on the Science Array. This
crude flatfield shows a weak structure of diagonal bands across the array and
some difference in sensitivity between the 4 quadrants (which are read out
separately). The gradient from top left to bottom right is due to a gradient in
the external illumination.
Dark Field. The dark current on the chip is
very low, 0.02 electrons per second or less at 80-90 K. The upper two quadrants
have rather more hot pixels than the lower but these pixels are not saturated
and consistently subtract out.
Image with a 2.4 um narrowband filter, quadrant 1
only, not flatfielded.
Image with a 2.4 um narrowband filter, quadrant 1
only, not flatfielded.
Author: Phil Lucas
This page last updated on Thursday 3rd September 1998